STC SE818GL

Supplemental type certificate · Shadin Avionics

Holder
Shadin Avionics · United States
Status
Current · Reissued
Status date
June 8, 2006
Applied
June 4, 1984
Product
Engine
Certification basis
Part 21
Data sheet
TCDSTC 5E-1

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of a Fuel Flow Transducer

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Type Certificate No. 5E-1.

Installation of a Fuel Flow Transducer in accordance with Shadin Report 4066 dated June 4, 1984 or subsequent FAA approved revision.

1) This approval should not be extended to other engines of this model that incorporate any other previously approved modification, unless it is determined that the interrelationship between this change and any other previously approved modification will introduce no adverse effect on the airworthiness of these engines.

2) If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Shadin Avionics 6831 Oxford Street St. Louis Park, MN 55426 5E-1 Make : Pratt and Whitney Model : R985-5, -13, -17, -19, -23, -25, -27, -39, -39A, -48, -50, -AN-1, -AN-3, -AN-1N1, -AN-2, -AN-4, -AN-5, -AN-6, -AN-6B, -AN-8, -AN-10, -AN-12, -AN-12B, -AN-14B, -AN-14BM1 Date of application : June 4, 1984

Date of issuance : September 6, 1984

Date reissued : June 8, 2006

( Signature) Charles L. Smalley Manager, Systems & Flight Test Branch Chicago Aircraft Certification Office

( Title)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
Pratt & Whitney DivisionMilitary R-985 SeriesTC 5E-1